B 4 N65317 From 337 Major Repair 2015 12 10

User Manual: B-4 N65317 From 337 Major Repair 2015-12-10

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US neP.knent

0l Trenspsrlation

Fede.+: Avialion

AdsHinisaratiffi

ililAJOR REPAIR A}IB ALTERATION

{Ai rframe, Powerplant, Propeller, or Appliaxce}

rorm Apgovet

OMB No. 2l?ff-0fl:ff

For FAA Use Gnly

Oflice ldentificaii0n

INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix *,

and disposilion oithis form. This report is required by law {49 U.S.C. 1421}-

for esch such virlation i$e**cn SOt Federal Aviali*r': Act cf 1958).

ard,AC 43-9-! {s. subsequent revision thsreof) fo. i.st.rctions

-ailure to reFort can result in civil pena*y nat tr exceed 51,0$0

{. Aircraft

Male

I'r 1a lri :l Model

F4 - PC.t

$erial Ns.

19,J

&l*tianelity and Regisiration Mark

r'.1 65,11 I

3. ffwiler

Nam6 i.As sftown ofl rcgr$fratron cedrficat4

;:ea:€r B._,;:rl:crr;aa It::g Club Itrr:

Address {.qs sf}srAfl &ri resisara*on ceftifreate)

:3: Ei:l ST.

."isedham, Ma.021!l

3. F(}r FEA ljse Onlv

4. lrn:1 ldentification 5= Type

Unii Make Model Serial No. Repair Alteraiian

\}RFRAME (As descnbecJ rn ltem 1 above)

}GW=RPLANI

lROFELLER

A?PLIANCE

Type

Manufactu.er

6. Cs]}:orin;ry Statemext

A. Aqency's Name 6ftd Addr€ss B= Kind afAEency C. C€rtific*te F,l{r.

.Ifrar=:r TruC--ru

2:2 E=-ch=:in,*n l*l.l .

_ioir:€. I-13 . it1i,,.:2

ll S CediflEle.l tule.har :.:)9444,-.)9

Forei. * Ce*ili€1ed A,,lechanlc

Certificaied Reoair Staiian

D. I cer':i:y ths: tale repai. andlor alteration made lo the rnil(s) ider:tiied in itern 4 abcve and described on ilie reverse or attachments herel*

have bee* made in accordance with the requi.ements *f Parl 43 of tire U.S. Federal Aviation Regulations and ihat lhe infermaticr:

fumisled hereil !s lrue and correct io the hesl of my knowledge.

uate

Cdi 1J

7. Approrg{for Retyfn TfSeMdE--

Fursuant lc the auihority given persons spe*lfied b*law, the unit rdgfiiified in ftem 4 was inspected in the mann*r prescribed by the

Administratorof :-eFederal AvialionAdmin;strationanda$ /7 l< APPROVED tf REJFCTED

: FAA alt. S:*ndards

I inspeclor

t AA I les!ilne-a

r Manufucturer

: Repair Stali0n

: lnspection Authorhation

: Person Approled by Transpori

I Canads Ai,tnrorthiness Group

ulnsr r$pec/ryl

Drte ofApproval er Rejecton

iir'74 ii.:

Ce.tificate Gr

Desigration No.

429+4e-?:;l '*"ff;:-':w

FAA Form 337 i12€s)

8. Description of Work Accomplished

flirro# space is req*ir*d. aiach addtlionat sheels, ldentify with aircraft natianality and registration rnarl< and date wark completed.)

Rem*ved prev;*L$ repair doubler to canopy hinge. Rivets were pulling through the skin a*d radiating cracks

were obserYed in the rivet holes.

Repaired torn out section { 1"x2" areai by inserting a i.8S0"xS", .050 u clannei} made up of 2024 T3 , ar:d riveting

in place with 19 CR3213-4-3 rivets acrcss the tap of the channel ar:d 6 CR3212-4-2 along the sides oi the channel

using the factory rivet hole locaiis.rs.

The Pilatus 84 Mair:teaa*ce ar:d Relair Manua! Do*ument No. 23-1 1-00-01482 was used as the repair guide.

As simiiar amounts ol material were .emoved from the previous repai: a *egligible weight change resulted.

:.: Additianal Sheets Are Attached

I.ISTISE

Weight and balsrce or opcralhg lir:dafian c$anges s&alJ &e entered in the apprap{iate ar-rcraff record An att€ration rnusf 0e

campatibl* with alt previous alferaiibns fo assuxe coafinaed conformity with the appliable ai"nvortirress r*quircments.

- u.s.G.=.c. 1990-7s1-753

' l'lliTi:'{ -

{

'i5 t,r.J.gtmer{ .

:x ,}lf r(n

/<if,oa /h/ro\1il

Ad.rLrl r trcflqr

MAJOII REPAIR AND ALTERATION. '' "'

(Ai rf ram e;' P i,iierpl an t, Pro pel I tirj' or np pl ia n ce)

^tr-*rt*,tr'"t*,ype allentrics.SeeFAR43.g,FAR43Append-ix.B'andAc43'9-1 (orsubsequenlrevisionthereof)forinstructions

and disposirion of this torm. This reporl is require d t, i;;?3.U- !ii' iizil itir'i"r-o tupotit"n resuliin a civil penalty nol to exceed S 1 000

for each such violation (Section 901 Fcrleral Aviation Act ol 1958)

PILT\TUS

f,i0

2. Owner

Narne fAs shown on reg,slration cetlilicate)

CREATER BOSTON SOARTNG CLUB

84-PC-i 1

IJatronality and Registration lu4ark

N653i7

,r,'tdr"tt fAs shown on regislralioti certittcale)

131 Bird St.

Needham, NjA .ofio'e

3. For FAA Use OnlY

Form APProYod

OMB No.2120{020

For FAA Urc

Office ldentilicalion

1. Aircrail

ATRFRAT.IE I .--

it ldentilicafion

Model I Serial I'Jo'

in ltem 1 abave)

5. Type

*-**( s describeC

Repair Alieratlon

PROPELLER

APPLIANCE

Type

tula"u factr re,

c Ccrtificate No

A. Agency's Name and Address

Alan Raymond

3 Bankowski St.

Sandwich, MA. 02563 I Certif icated FeP'rir Siation

-_--1--

I Manulacturer

U.S- Certilica ted l"'lechanrc

Foreiqn Cerlilicated l"lechanrc L942i 41.9

D" *,, **''" ,.n*,.. "^"or arter.rtion made to the unit(s) identilied in item 4-above and described on the reverse or attachments hereto

have bcen made an accordance wirh the requiremenrf oi p"., o: o( the u.s. Feoeral Aviation Regulalrons and ihat the inlormation

furnishodhereinistrueandcorrecltothebeStofmyknowledge.

Date

March 26,L992

s.c^"t,Ail^,r."-Gi"c'fJ \ ) |

f}tc;..-\ \dr"-t-^-]-

'I'APP@

low,thes.ljo-"gl):o^initem4wasinSpec1edinthernannerpreScribedbythe

Other (SPeci/Y)

6Yl

FAA Flt. Standards

lnspirctor Manrrlaclurer lnspection Authorization

Repeir Ststion Person AgProved bY Transport

Canada Alrworthiness GrouP

Date of Approva!.or Reiection

March 26 '1992

Certilicate or ,

Oesignation No.

- 1(i28408

FAA Form 337 trz-mt

8. Oercripllon ol Work Accompltshed tark and dalo work contpleled-)

(lt rnc,rsspaco rs roquired, attach additional snsals.'ldon lily wilh aircrall nalionatity and tegisltalion n

)

P.e inf orce.<l 1or,,er section of. li3 bulkhead with doubler rabricai-eri from'

2024 T 3 Alclad .040 and installed, usinS existing ri-vet holes and edge

rj-vets placed, using standard nlfg. spaci-ng and edge distance (see rJrar"ing) '

Data ref. Ac 43-131t\, ch. 2, par' l-00, sub par' F'

Fleplaceci cleci< sliit.t betI.IeeIi ii 3 and lr bu1]<heads ' 'Skin f abricated irom 202lrT3

alclacl .040 ancl installed us j-ng existi-ng rivet holes '

PatciteC i.roIc in fuselage be11y using practices as outlined in Sec ' 1r ' Fig

of pila'rus Blr maintenance and repair manual '

l'.epairs do no-u ref lect arrl- l{eight & Balance change '

.,-..-r+: )lor':-i,il;,_Iolaa:-+s_-fr':r':'11. _

{

l/ ns\

I/-l

lr r)

l/ z-( \

/ \ /N..t

Lzt \

'.'Yl

D Additional Sheels Aro Attached

B 4 N65317 From 337 Major Repair 2015 12 10

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